SEA89FA157

NTSB accident investigation · Beech C35 · Sandy, OR · August 27, 1989

Accident · FatalField investigationFinal report
Date
August 27, 1989, 16:30 local (23:30 UTC)
Place
Sandy, OR
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N5916CBeech C35
Weather
Visual (VMC) · Day
Status
Completed · report January 23, 1992
Report
Approved by Office Director
FAA report
19890827031699A
Case key
40933

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The loss of engine power due to the separation of the bolt connecting the throttle rod to the carburetor throttle arm and an inadequate annual inspection performed 5 flight hours prior to the occurrence. Contributing factors were obstructions in and around the only open field available for the forced landing.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - mech failure/malfClimb - to cruise
Throttle/power lever,linkage - not safetiedCause
Maintenance,annual inspection - poorOther maintenance personnelCause
Throttle/power lever,linkage - disconnectedCause
Fluid,fuel - starvationCause
Forced landingApproach - vfr pattern - final approach
In flight collision with terrain/waterApproach - vfr pattern - final approach
Object - fenceFactor
Object - tree(s)Factor
Terrain condition - mountainous/hillyFactor
Terrain condition - open fieldFactor

Analysis

The engine lost power shortly after takeoff and a forced landing was made in an open field. The airplane collided with the terrain and cartwheeled. The bolt connecting the throttle arm to the throttle rod end was missing. A bolt identified as the proper type for this connection was found laying against the firewall. The bolt is supposde to be secured with a castellated nut and a cotter pin. Neither the nut nor the cotter pin was found. The bolt was not damaged. An annual inspection was performed 5 flight hours prior to the accident. The open field used for the forced landing is surrounded by 100 ft trees, with barbed wire fences 300 to 400 ft apart. Initial ground impact mark was located 64 inches from a fence.

Aircraft

Registration
N5916C
Reported as
Beech C35
Category
Airplane
Serial number
D-3276
Airframe hours
3,725
Engine
Continental E-225-8, 225 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Wesley, Greene S.
Registered owner
Helm, John C
Airworthiness certificate
Standard, Normal
Last inspection
Annual · August 3, 1989 · 5 hours before
Departed
03S · Sandy, OR
Destination
7S3 · Hillsboro, OR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
55
Certificates
Flight instructor, Commercial, Airline transport
Airplane ratings
Single-engine sea, Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
4,894 total · 4,517 as pilot in command · 59 in the last 90 days · 22 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
10° at 5 knots
Visibility
40 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 63 °F
Altimeter
30.00 inHg
Observed at
PDX, 18 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.